Object 68/1 - 68/40
Container
Contains 33 Results:
Calculation of the performance of aggregates that were developed from the aerodynamic basic form A4, 1942-05-01
File — Object: 68/1 - 68/40, Folder: Arch 68/24
Dates:
1942-05-01
In-flight skin and payload tip heating of various A8 and A9 designs, 1942-06-16
File — Object: 68/1 - 68/40, Folder: Arch 68/25 (Copy)
Dates:
1942-06-16
Testing of the A7 ejector glider in the Braunschweig 8m wind tunnel
File — Object: 68/1 - 68/40, Folder: Arch 68/27
Dates:
1920 - 1970
The effect of the ailerons of the fin projectile A4 V12/c with transverse airflow, 1942-10-13
File — Object: 68/1 - 68/40, Folder: Arch 68/28
Dates:
1942-10-13
The influence of the crosswind on the start of A9, 1942-10-13
File — Object: 68/1 - 68/40, Folder: Arch 68/29
Dates:
1942-10-13
Research into the possibility of achieving a firing range of 160 with the heavy mortar "Thor", 1943-01-29
File — Object: 68/1 - 68/40, Folder: Arch 68/30
Dates:
1943-01-29
Pressure point migration on the A9 unit during the transition to supersonic, 1943-05-25
File — Object: 68/1 - 68/40, Folder: Arch 68/31
Dates:
1943-05-25
Analysis of a preliminary project for GI, 1943-03
File — Object: 68/1 - 68/40, Folder: Arch 68/32
Dates:
1943-03
Engine construction project "Waterfall." This report consists of 8 pages of text and 6 figures, 1943-07-16
File — Object: 68/1 - 68/40, Folder: Arch 68/35 (Copy)
Dates:
1943-07-16
Study of the trajectory of a body parachuted from a height of 60 km, 1943-04-28
File — Object: 68/1 - 68/40, Folder: Arch 68/37
Dates:
1943-04-28